N530AS
Service difficulty reports · 357
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N530AS' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N530AS' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ASAA2019110131216Warning System · false activationHF2 "FAIL" DISPLAYED WHEN TESTING HF COM. GROUNDED - YES. PERFORMED BITE OF HF2 SYST REF B737-800 AMM 23-11-00-810-801 NO FAULTS FOUND. PERFORMED HF OPS TEST REF AMM 23-11-00-710-801 OPS CHECKS GOOD. DISPLAY NO LONGER SHOWS "FAIL". FUEL TRUCK REMOVED FROM AREASDR ASAA2019091230702Exciter · failedAPU FAULT LIGHT ILLUMINATED DURING START. FAULT LIGHT EXTINGUISHED AFTER 5 MINUTES. GROUNDED - YES. APU WOULD NOT START, TRIED TWICE. REMOVED AND REPLACED APU EXCITER UNIT IAW AMM 49-41-31-000-801 AND 49-41-31-400-801, ETOPS GROUND FUNCTIONAL CHECK GOOD IAW AMSDR ASAA2019071130055Pressure Switch · failedRIGHT FUEL FILTER BYPASS ON CLIMBOUT FROM AIRPORT. LIGHT EXTINGUISHED AFTER SHUT DOWN. GROUNDED - YES. REMOVED AND REPLACED FFDPS REF AMM 73-34-01. OPS CHECK NORMAL. PERFORMED EEC TEST AMM TASK 73-21-00-700-804-F00. TEST PASS. NO DEFECTS NOTED. PERFORMED IDLE SDR ASAA2019070829969Drive Unit · vibrationWX FAIL ANNUNCIATED ON BOTH ND DISPLAYS COUPLED WITH HIGH FREQUENCY VIBRATION FELT IN FLIGHT DECK FLOOR. VIBRATION CEASED WITH WEATHER RADAR DESELECTED. GROUNDED - YES. REPLACED WX ANTENNA DRIVE UNIT PER AMM 34-43-11. OP TEST NORMAL PER AMM 34-43-00.SDR ASAA2019070329909Warning System · false activationWX RADAR INOP. WXR FAIL AND ANT AND PWS FAIL ANNUNCIATED ON INBOARD DU. GROUNDED - YES. CYCLED A/C POWER IN REF TO AMM 20-60-99. PERFORMED B737-800 FIM 34-43 TASK 801 NO FAULTS NOTED.SDR ASAA2019061399660Warning Light · false activationAT CRUISE LFT CTR BOOST PUMP LIGHT CAME ON STEADY WITH 900 LBS. FUEL IN CTR TANK. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 28-22 TASK 801. LEFT CENTER BOOST PUMP OPS CHECK GOOD. ALSO REF 737 SYSTEMS HAND BOOK. FUEL, SECTION 12.010 PAGE 11.SDR ASAA2019060629595Pump · low pressureSHORTLY AFTER TAKE OFF #2 MAIN TANK LOW PRESSURE LT (AFT) ILLUMINATED CHECK LIST COMPLETED TURNED PUMP OFF. GROUNDED - YES. ON DEFERRAL.SDR ASAA2019053029538Connector · looseAFT #2 MAIN TANK BOOST PUMP INOP. FAILED @ FL340 30 MINUTES INTO FLIGHT. GROUNDED - YES. ON INITIAL TROUBLESHOOTING, FOUND GFI RELAY NOT TRIPPED. ACCOMPLISHED FIM TASK 28-22 TASK 816 "NO 2 TANK AFT BOOST PUMP CIRCUIT BREAKER OPEN-FAULT ISOLATION". ON FUEL TANKSDR ASAA2019050729395Probe · failedREF L/P 11876920, ACCOMPLISH #2 ENGINE EGT PROBE CLEANING. ACCOMPLISH EEC BITE TEST BETWEEN 10-20 CYCLES DURING RETEST IF FAULT EXISTS ON ANY OF THE LAST TEN LEGS PERFORM ELECTRICAL CHECKS ON ASSOCIATED SECTOR AND HARNESSES WITH IN 5 DAYS. GROUNDED - YES. INTESDR ASAA2019041979047Terminal Block · unsecureAT LEVEL CRUISE FLIGHT AUTOPILOT A DISENGAGED. AUTOPILOT A WOULD NOT RE-ENGAGE. COMPLETED FLIGHT ON AUTOPILOT B. GROUNDED - YES. DFCS SHOWS NUMEROUS FAULTS ASSOCIATED WITH SMYDC-1 MSG 22-11081 FOR CH A THROUGH OUT FAULT HISTORY. NO SMYDC FAULT ON CDS BITE OR HSDR ASAA2019041729027Indicator · out of toleranceCAPT F/D PITCH BAR NOT IN VIEW. GROUNDED - YES. T/S REF B737-800 FIM 22-11 TASK 801, AMM 22-11-00-740-801. OPS CHECK GOOD.SDR ASAA2019030528658Threshold · corrodedAFT CARGO DOOR THRESHOLD WEB HAS CORROSION IN PREVIOUS BLENDOUT. GROUNDED - YES. REMOVED CORROSION IAW SRM 53-60-15. ORIG THICKNESS 0.050 REMOVED 0.012 REMAINING MAT 0.038 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15. TOOL #T82250. REMOVED WEB IAW SRM 51-40-02. SDR ASAA201902128151Lubrication Unit · stuckFWD SUMP SEALING SPOOL ON LUBE UNIT STUCK OPEN AND SEALS ARE CUT, #1 ENGINE. GROUNDED - YES. REPLACED #1 ENGINE LUBE UNIT PER B737-800 AMM 79-21-01. LK CK GOOD.SDR ASAA2019020128022Case · damagedDURING REPAIR OF NR 1 ENGINE FLANGE B SCALLOPED FAN CASE FOUND CASE NOT REPAIRABLE. GROUNDED - YES. REMOVED & REPLACED NR 1 ENGINE. ACCOMPLISHED NR 1 ENGINE DUCT PURGE PER PWRPL-71EA-11276. COMPLETED MIG-2C 316258.SDR ASAA2019012827967Mount · crackedWHILE ACCOMP INLET & FAN BLADE INSP NR 1 ENGINE S/N 892938 FOUND "B" FLANGE SCALLOP MOUNT, OTBD POSN FOR FWD FIRELOOP TRANSPONDER CRACKED. GROUNDED - YES. REMOVED TWO EACH BRACKETS ON EACH SIDE OF DAMAGED AREA. COMPLETED STEPS 5 - 6 OF TASK CARD SBCFM56-7B-72-SDR ASAA2019011827879Wire Harness · failedREF LOG PAGE 12060713 TO ACCOMPLISH EEC BITE TEST FAULT HISTORY BETWEEN 10-20 CYCLES FOR NR 2 ENGINE. FAULT 77-10852 IS STILL ACTIVE. REQUIRES CORRECTION WITHIN 5 DAYS. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENG CJ9 HARNESS, AND NR 2 ENGINE S2 EGT PROBE IAWSDR ASAA2019011827873Unknown · malfunctionedAPU FAILED TO START AFTER LANDING W/ "APU FAULT" LIGHT ILLUMINATED. GROUNDED - YES. MAINTENANCE MESSAGE 49-41012 NO APU ROTATION SHUTDOWN SHOWS ON LAST TWO START ATTEMPTS WITH NO CURRENT FAILURES. FOUND FAULTS TO BE INTERMITTENT REF FIM 49-40 TASK 803 AND FIM SDR ASAA2019011127740Probe · intermittentDIAGNOSTICS REPORTS NR 2 ENGINE TREND DATA SHOWS A SHIFT IN EGT INDICATION ERRORS ARE SUSPECT. GROUNDED - YES. DUE TO HISTORY, REMOVED AND REPLACED THE T49.5 S2 PROBE REF AMM 77-21-01/401. PERFORMED EEC TEST REF AMM TASK 73-21-00-700-804-F00 - OPS CK GOOD.SDR ASAA2019010627695Unknown · malfunctionedAFTER ENGINE START ATTEMPTED TO PUT GEN1 ON THE BUS WE COULD NOT ESTABLISH ELECTRIC W/ GEN 1 AND SAW THE TR UNIT LIGHT WAS ILLUMINATED. GROUNDED - YES. INTERROGATED CREW FOUND EXTERNAL POWER HAD AN INTERRUPTION RESET TRU 1,2,3 C/BS AFTER SHUTTING DOWN POWER, RSDR ASAA2018121067259Actuator · inoperativeAFTER ENGINE START ON RECALL THE RIGHT PACK LIGHT CAME ON AND WENT OUT WHEN MC WAS PRESSED. GROUNDED - YES. PERFORMED PACK TEMP CONTROL BITE TEST REF FIM 21-62 TASK 801. #2 CONTROLLER LOG FAULT RAM AIR ACTUATOR. WILL NOT RESET. REMOVED/REPLACED #2 RAM AIR ACTUSDR ASAA2018120627234Harness · damagedNR 2 ENGINE J9 HARNESS DAMAGED. GROUNDED - YES. REPLACED THE NR 2 ENGINE J9 HARNESS PER AMM 73-21-06/401. ACCOMPLISHED FADEC SYSTEM TEST REF AMM 73-21-00-700-802-F00 5D(3)(A),(B),(C) AND (E). ALL RELATED TESTS PASSED.SDR ASAA2018120527239Connector · damagedWHILE INTERROGATING NR 2 ENGINE BITE RECENT FAULTS SHOWN: 75-20362, 75-10462, 75-30412, 75-20462. GROUNDED - YES. DURING GVI, FOUND CONNECTORS DP1003 LOOSE AND DIFFICULT TO REMOVE. CONNECTOR DP1003 AND RECEPTACLE AT HPTACC VALVE IS FOUND DAMAGED REF FIM 75-21 SDR ASAA2018120527232Wire Harness · damagedNR 2 ENGINE MW0311 HARNESS DAMAGED. GROUNDED - YES. REPLACED THE NR 2 ENGINE MW0311 HARNESS PER AMM 73-21-06/401. COMPLETED ALL TEST AND AVM TEST AMM TASK 77-31-00-710-801-F00. CKS NML.SDR ASAA2018102426591Control Panel · defectiveWX RADAR CONTROL PANEL AUTO/MAN PUSH-PUSH SWITCH WILL NOT HOLD SELECTED TO AUTO. (THE SWITCH "HOLDS" IN AUTO BUT THE RADAR STAYS IN MANUAL). GROUNDED - YES. REMOVED AND REPLACED WEATHER RADAR CONTROL PANEL PER AMM REF 34-43-91-000-801/34-43-91-400-801. OP'S CKSDR ASAA2018100826389Control Valve · failedLEFT "PACK" LIGHT ILLUMINATED ON RECALL AFTER START. GROUNDED - YES. NR 1 PACK TEMP CONTROLLER FFR SHOWS TCV THIS PACK. FAULT HAS HISTORY. REMOVED AND REPLACED LEFT HAND TEMP CONTROL VALVE ASSY IAW AMM 21-51-10. SYSTEM OPS CHECK GOOD. GROUND VERIFICATION GOOD.SDR ASAA2018092826308Warning System · false activationAFTER MASTER CAUTION RECALL THE LT PACK LIGHT ILLUMINATED. THE LIGHT CLEARS WITH A RESET. GROUNDED - YES. RELEASED PER MEL 21-32B LT PACK PRIMARY TEMP CONTROL INOP FIM 21-62 TASK 830. LEFT PACK/ ZONE TEMP CONTROLLER HAS FAULT "THIS PACK, TCV" PERFORMED PZTC BISDR ASAA2018091426108Module · failedAPPROXIMATELY ONE HOUR INTO FLIGHT IN LEVEL CRUISE AT FL 360 THE A AUTOPILOT DISENGAGED. WAS ABLE TO REENGAGE A AUTOPILOT. AFTER TEN SECONDS A AUTOPILOT AGAIN DISENGAGED. SWITCH TO B AUTOPILOT WITH NORMAL OPERATION. GROUNDED - YES. PERFORMED DFCS BITE REF FIM SDR ASAA2018090425979Warning System · false activationAUTO FAIL AND ALTN LIGHTS ILLUMINATED. GROUNDED - YES. CYCLED SWITCH ON PRESS CONTROL PANEL, LIGHTS CLEARED - ACCOMPLISHED BITE OF THE DIGITAL CABIN PRESSURE CONTROLLERS, REF FIM 21-31 TASK 801 - CONTROLLER NR 2 SHOWED CONTROL LRU FAILURE IN EXISTING FAULTS, NSDR ASAA201808135749Blade · damagedNR 2 ENGINE FAN BLADE ROOT HAS CU-NI-IN COATING MISSING, AND WAS OUT OF LIMITS. ALL BLADES EXCEPT NR 4 & 16 IAW T/C 78472002. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE FAN BLADES EXCEPT NR 4 AND 16 IAW T/C 78472002.SDR ASAA2018073025529Control Valve · failedAFTER ENGINE START LEFT PACK LIGHT ILLUMINATES WITH MASTER CAUTION RECALL AND EXTINGUISHES WITH RESET. GROUNDED - YES. REMOVED & REPLACED LEFT PACK TEMP CONTROL VALVE REF AMM 21-51-10. BITE AND OPS CHECK GOOD.SDR ASAA2018072325522Actuator · failedLEFT PACK CAUTION ILLUMINATES WITH MASTER CAUTION RECALL AND EXTINGUISHES WITH RESET. GROUNDED - YES. REMOVED AND REPLACED THE LT RAM AIR ACTUATOR ASSY REF AMM 21-51-21-000-800 AND AMM 21-51-21-400-801. OPS CHCKS OK.SDR ASAA2018072425508Warning System · false activationLEFT A/C PACK ILLUMINATE ON RECALL ON DESCENT CHECKLIST, EXTINGUISHES WITH/ON MASTER CAUTION RESET. GROUNDED - YES. NR 1 PACK ZONE TEMP CONTROLLER SHOWS RAM AIR ACTUATOR ON BIT, GREEN FOR PREVIOUS & VERIFY, FAULT RESET REF FIM 21-62 TASK 801 & 837.SDR ASAA2018070225274Unknown · malfunctionedAP A DISCONNECTED TWICE IN CRUISE. ALSO CAPT PITCH BAR WAS OUT OF VIEW WITH AP A IN USE. GROUNDED - YES. FAULT FLIGHT REVIEW SHOWED LEG 11 WITH 13 FAULTS RELATING TO NR 1 SMYD. NR 1 SMYD SHOWED FAULT MESSAGE 22-21001 LEGS 11, 33 & 40 ON THE GROUND AND INTERMITSDR ASAA2018062505166Warning Light · false activationON PRESSING THE MASTER CAUTION RECALL AT THE TOP OF DESCENT, OBSERVED AMBER LT PACK LIGHT ILLUMINATED. FOLLOWED QRH PROCEDURES AND PACK LIGHT EXTINGUISHED AFTER MASTER CAUTION RESET. QRH STATES NO FURTHER ACTION REQUIRED. ALL OTHER SYSTEMS FUNCTIONING NORSDR ASAA2018061325062Fmc · malfunctionedLEFT FMC FAILED. GROUNDED - YES. ACCOMPLISHED FIM 34-61TASK 807. NO FAULTS NOTED. NO HISTORY.SDR ASAA2018052724810Warning System · false activationL PACK LITE CAME ON WHEN MASTER CAUTION RECALL PERFORMED AFTER ENGINE START. GROUNDED - YES. RAN BOTH PACKS- NO FAULTS NOTED. T/S REF FIM 21-61 TASK 801. THIS REMOVES MEL 21-32B.SDR ASAA2018051824695Autoland Sys · malfunctionedON SHORT FINAL, AUTOLAND APPROACH, ACFT DEVIATED LEFT OF CENTERLINE AND APPROACH WARNING INDICATION DISPLAYED. CRITICAL AREA WAS PROTECTED DUE TO WEATHER. XTM RATE EXCEED DISPLAYED IN RECORDED FAULTS AFTER LANDING. ACFT GROUNDED. BITE CHECKED IAW FIM 22-SDR ASAA2018042824413Control Valve · failedAFTER START CHECKLIST, THE LEFT PACK LIGHT ILLUMINATED, MC RECALL. EXTINGUISHES WITH MC RESET. ACFT GROUNDED. PERFORMED CABIN TEMP CONTROLLER BITE IAW FIM 21-61-00-810-801, FLIGHT DECK TRIM VALVE FAILED ON ZONE TEMP CONT 2. REMOVED AND REPLACED THE ZONE TRSDR ASAA2018042724436Hmu · leakingWHILE ACCOMPLISHING AN IDLE NR 2 ENGINE RUN, FOUND FUEL DRIPPING FROM THE HMU JUST ABOVE FWD THE CONNECTOR. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE HMU IAW N8473000, N8473001. TESTED IAW AMM 71-00-00-800-811-F00, TABLE 502.SDR ASAA201804304435Heater · leakingNR 2 ENGINE SERVO FUEL HEATER FAILED A LEAK CHECK 3A. ACFT GROUNDED. REMOVED THE NR 2 ENGINE SERVO FUEL HEATER IAW AMM 73-11-07-000-801. INSTALLED A SERVICEABLE FUEL HEATER IAW AMM 73-11-07-400-801-F00. TEST ACCOMPLISHED IAW AMM 71-00-00-800-811-F00, TABLESDR ASAA2018040124092Connector · dirtyDIAGNOSTICS REPORTED THE NR 1 ENGINE TREND DATA SHOWS A SHIFT IN DELTA EGT AND EGT HOT DAY MARGIN ALL OTHER PARAMETERS NORMAL. EGT INDICATION ERRORS ARE SUSPECT. ACFT GROUNDED. ACCOMPLISHED A NR 1 ENGINE EGT CONNECTOR CLEANING IAW AMM 77-21-00-140-801, ALL SDR ASAA2018032123997Control Valve · failedCONTROL CABIN ZONE TEMP LIGHT ILLUMINATES DURING RECALL. THE ZONE TEMP LIGHT EXTINGUISHED ON MASTER CAUTION RESET. ACFT GROUNDED. CONFIRMED FAULT, THE NR 2 PACK/ZONE TEMP CONTROLLER BITE IAW AMM 21-61-00-700-806-002, SHOWS HARD FAIL FLIGHT DECK TCV V143. SDR ASAA2018031723979Egt Indication · out of toleranceFAULT CODE APPEARED ON THE NR 2 ENGINE, FAULT CODE 77-20862, BOTTOM LEFT EGT SIGNAL, T495S3 IS OUT OF RANGE. ACFT GROUNDED. T49.5 S3 PROBE CHANNEL B FAULTING AND SHOWS DASHES ON INPUT MONITORING. FAULTS SHOWN ON EVERY LEG. J10 HARNESS RANG OUT WITH NO RESULSDR ASAA2018030923800Warning Light · false activationAFTER ENGINE START CHECKLIST. ON INITIATING MASTER CAUTION RECALL, THE LT PACK LIGHT ILLUMINATED, LIGHT EXTINGUISHED WHEN MASTER CAUTION SYSTEM WAS RESET. ACFT GROUNDED. ACCOMPLISHED FIM 21-61 TASK 801. TCV FAULT CLEARED. RECALL CHECKED GOOD.SDR ASAA2018030323734Filter · dirtyZONE TEMP CONTROL AMBER LIGHT ILLUMINATED DURING RECALL. RESETS WITH MASTER CAUTION. ACFT GROUNDED. PERFORMED PACK ZONE TEMP BITES, FLT DECK TRIM VLV FAULT SHOWN. CLEARED FAULT, SUBSEQUENT BITES SHOW NO FAULTS. FOUND CABIN TEMP SENSOR FILTER DIRTY, CLEASDR ASAA2018022323696Wire Harness · intermittentWHILE PERFORMING FMC CDU INTERROGATION, THE FOLLOWING FAULT DISPLAYED FOR THE NR 2 ENGINE. MESSAGE 77-20862. BOTTOM LEFT EGT SIGNAL IS OUT OF RANGE (T495S3) FLT LEGS 0, 1, 2, 3. ACFT GROUNDED. NR 2 ENGINE T49.5 S3 PROBE CHANNEL B FAULTING AND SHOWS DASHES OSDR ASAA2018022123664Warning Light · false activationELEC LIGHT ILLUMINATED AT GATE. ACFT GROUNDED. POWERED DOWN ACFT, PERFORMED BITE CHECK AND NOTED INTERMITTENT SPCU FAULT DUE TO GROUND POWER ISSUE, CLEARED FAULT AND ELEC LIGHT EXTINGUISHED IAW FIM 24-31 TASK 801, AND FIM 24-34 TASK 802.SDR ASAA2018021823597Circuit Breaker · trippedL1 WINDOW OVERHEAT LIGHT ILLUMINATED IN FLIGHT. COMPLIED WITH QRH, LIGHT REMAINED ILLUMINATED WHEN TURNED BACK ON. COMPLIED WITH REMAINING QRH PROCEDURES. ACFT GROUNDED. FOUND THE CIRCUIT BREAKER OPEN. RESET THE CIRCUIT BREAKER IAW AMM 20-60-01 NORMAL OSDR ASAA2018020423397Probe · malfunctionedNR 2 ENGINE, T49.5 EGT PROBES BEFORE AND AFTER CLEANING READOUT, EGT PROBE S3 SHOWS DASHES. ACFT GROUNDED. PERFORMED FIM 77-31 TASK 803. CLEANED THE CONNECTORS IAW AMM 77-21-00. PERFORMED RESISTANCE CHECK OF J10 TO DP1010, RESISTANCE CHECKED GOOD. PERFORMSDR ASAA2018011723182Wire Harness · faultedNO APU BLEED AIR DUCT PRESSURE. ACFT GROUNDED. ACCOMPLISHED AN APU BITE, FAULTS LAST 90 DAYS, 49-41012, AND 49-31016. REMOVED & REPLACED THE APU WIRE HARNESS. OPS GOOD. GROUND VERIFICATION SUCCESSFUL. IAW AMM 49-61-00-700-801, AND 49-61-01/401.
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